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ModifiedKeplerianElementsComputeMeanAnomaly Method

Computes the mean anomaly based on the current Keplerian position.

Namespace:  AGI.Foundation.Coordinates
Assembly:  AGI.Foundation.Core (in AGI.Foundation.Core.dll) Version: 19.1.398.0 (19.1.398.0)
public double ComputeMeanAnomaly()

Return Value

Type: Double
The current mean anomaly (radians).
InvalidOperationExceptionIn the case of a hyperbolic orbit, the true anomaly 'v' is bound within: -Pi+ Acos(1/e) < v < Pi - Acos(1/e). Otherwise, the method throws an exception.
See Also